Takeoff Performance - Robin DR400 Series Pilot Operating Handbook

TAKEOFF PERFORMANCE

At max. take-off weight 980 kg (2161 lb), without wind, flaps in takeoff
position, engine full power
Conditions

No wind, flaps in takeoff position (1
brakes before release
 Level, dry, asphalt runway
 Rotation speed v
 Lift off speed Vlof ...................................................... 105 km/h (57 kt)
 Speed at 15 m (50 ft) height obstacle clearance ...... 113 km/h (61 kt)
Pressure
ISA conditions
Altitude
[ft]
To lift-off
0 240
1000 260
2000 270
3000 280
4000 300
5000 310
6000 330
7000 360
8000 390
9000 410
Table 5-2 Takeoff distance (m) at 980 kg (MTOW)
Page 5 - 2
Supplement
DR400/180R, DR400/200R, DR400/RP
......................................................... 96 km/h (52 kt)
r
Take off distance [m] at 980 kg (2161 lb)
to 50 ft
height
440
470
490
510
540
580
620
690
760
810
POH DR400/120D,
st
notch), engine full power on
ISA + 10°C
to 50 ft
To lift-off
height
260 480
270 500
290 530
300 550
320 580
330 620
350 660
380 730
410 810
430 850
DR400/140B,
ISA + 20°C
to 50 ft
To lift-off
height
280 520
290 540
310 570
320 590
340 630
360 670
380 720
400 790
430 880
450 930
Issue 3 – July 2014